What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Pilot stated: during landing on runway 35 a gust of wind forced the aircraft to the left off the paved runway onto the grass. The pilot stated that there was a helicopter that he was heading towards and attempted a go around. While attempting to climb the aircraft stalled and induced a hard landing onto the main landing gear and nose of the aircraft. The tail proceeded to rise up into the air, turned the aircraft 180 and dropped on the tail landing gear before coming to rest.
Markings on the ground showed aircraft heading through the grass was approximately 25 to 30 degrees to the runway. There was a short area in the grass with no tire wheel marking imprint, then tire marking and impact markings from the main landing gear and rotating propeller which were approximately 25 to 30 feet in area.
Damage to the aircraft consisted of propeller blades bent backwards, lower engine cowling dent. The left and right main landing gear completely separated from the fuselage and twisted. The main landing gear attaching hardware were sheared.
As the FAA filed it
PILOT STATED: DURING LANDING ON RUNWAY 35 A GUST OF WIND FORCED THE AIRCRAFT TO THE LEFT OFF THE PAVED RUNWAY ONTO THE GRASS. THE PILOT STATED THAT THERE WAS A HELICOPTER THAT HE WAS HEADING TOWARDS AND ATTEMPTED A GO AROUND. WHILE ATTEMPTING TO CLIMB THE AIRCRAFT STALLED AND INDUCED A HARD LANDING ONTO THE MAIN LANDING GEAR AND NOSE OF THE AIRCRAFT. THE TAIL PROCEEDED TO RISE UP INTO THE AIR, TURNED THE AIRCRAFT 180 AND DROPPED ON THE TAIL LANDING GEAR BEFORE COMING TO REST.
MARKINGS ON THE GROUND SHOWED AIRCRAFT HEADING THROUGH THE GRASS WAS APPROXIMATELY 25 TO 30 DEGREES TO THE RUNWAY. THERE WAS A SHORT AREA IN THE GRASS WITH NO TIRE WHEEL MARKING IMPRINT, THEN TIRE MARKING AND IMPACT MARKINGS FROM THE MAIN LANDING GEAR AND ROTATING PROPELLER WHICH WERE APPROXIMATELY 25 TO 30 FEET IN AREA.
DAMAGE TO THE AIRCRAFT CONSISTED OF PROPELLER BLADES BENT BACKWARDS, LOWER ENGINE COWLING DENT. THE LEFT AND RIGHT MAIN LANDING GEAR COMPLETELY SEPARATED FROM THE FUSELAGE AND TWISTED. THE MAIN LANDING GEAR ATTACHING HARDWARE WERE SHEARED.